F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 1/48 (2006.01) F02K 1/38 (2006.01) F02K 1/46 (2006.01) F02K 1/80 (2006.01)
Patent
CA 2693844
An exhaust nozzle for a gas turbine engine includes a modular chevron (54). The chevron includes dual skins (56, 58) fixedly joined together at a base flange, and at a rim (72) extending along the trailing edge (66) of the chevron between the base (64) and apex (62) thereof.
L'invention concerne une tuyère d'échappement pour une turbine à gaz comprenant un chevron modulaire. Ce chevron comprend des revêtements doubles liés ensemble de manière fixe au niveau d'une bride de base, et d'un rebord s'étendant le long du bord de fuite du chevron entre la base et le sommet de celui-ci.
Johnson Michael Robert
Nye Christopher Joseph
Tisdale Rudolph Morris
Uhler Gregory Allen
Company General Electric
Craig Wilson And Company
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